US3643320A - Method of mounting an automobile engine - Google Patents
Method of mounting an automobile engine Download PDFInfo
- Publication number
- US3643320A US3643320A US37556A US3643320DA US3643320A US 3643320 A US3643320 A US 3643320A US 37556 A US37556 A US 37556A US 3643320D A US3643320D A US 3643320DA US 3643320 A US3643320 A US 3643320A
- Authority
- US
- United States
- Prior art keywords
- bolt
- engine
- slots
- bushing
- clamping members
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F1/00—Springs
- F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
- F16F1/38—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers with a sleeve of elastic material between a rigid outer sleeve and a rigid inner sleeve or pin, i.e. bushing-type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K5/00—Arrangement or mounting of internal-combustion or jet-propulsion units
- B60K5/12—Arrangement of engine supports
- B60K5/1291—Supports comprising stoppers
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49616—Structural member making
- Y10T29/49622—Vehicular structural member making
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49904—Assembling a subassembly, then assembling with a second subassembly
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49947—Assembling or joining by applying separate fastener
- Y10T29/49948—Multipart cooperating fastener [e.g., bolt and nut]
- Y10T29/49952—At least one part is nonmetallic
Definitions
- a voided bushing assembly comprises an electric bushing radially spacing and bonded to an outer tubular housing member of oval cross section and a coaxial inner tubular support member.
- the outer member is tightly secured by a forced fit within a pair of closely conforming oval holes in a pair of axially spaced channel sides respectively of a one-piece channel-shaped engine bracket secured to the engine.
- a one-piece channel-shaped body bracket associated with each bushing assembly has a pair of bracket arms spaced axially to receive the bushing assembly therebetween.
- a pair of upwardly opening guide slots within the latter arms respectively receive the axially opposite ends of a bolt in supported relationship on their bases, the bolt being releasably confined coaxially by friction within the inner tubular member.
- Enlarged clamping members at opposite ends of the bolt axially outward of the slotted bracket arms and oversize with respect to the slots to prevent passage therethrough are adjustable axially with respect to each other by screw action to clamp the latter arms tightly against the bushing assembly therebetween.
- Flanges of the latter arms closely overlie the tightened clamping members to limit their movement from the slot bases, but without interfering with their adjustability.
- This invention relates to an improved vibration damping mounting structure and method for mounting an automobile engine on a vehicle body and has for an important object the provision of an engine mounting which is particularly simple and economical in structure and application, which utilizes a voided bushing to optimum advantage to obtain a fail-safe structure in the event of bushing deterioration, to facilitate tuning and vibration isolation to accommodate engine modifications, to provide a positive resilient engine support for limiting all components of engine movements, and in particular to reduce engine roll significantly to approximately one-third of former requirements for comparable engine mountings without sacrificing vibration-absorbing qualities.
- bushing assembly comprising inner and outer tubular members having parallel axes and spaced by an intermediate elastic bushing of rubberlike material.
- the outer tubular member is forced into axially spaced aligned openings within the paired channel sides of a one-piece channel-shaped engine bracket adapted to be secured in predetermined fixed position to one side of the engine with the axes of the tubular members extending longitudinally of the automobile body.
- the outer tubular member is out-of-round and preferably of oval cross section conforming to the shape of the aligned bracket openings and dimensioned to effect an interference fit therein at its axially opposite ends, whereby relative rotation between the bushing assembly and engine bracket is prevented.
- the above-described structure provides a fail-safe mounting in the event of deterioration of the elastic bushing, wherein the bolt shank and bushing assembly are closely confined against axially endwise movement by the channel sides or arms of the body bracket, against vertical movement by the bases of the axially spaced slots and by the clamping members, and against lateral movement by the sides of the slots.
- the instant structure materially facilitates mounting of the automobile engine on the body.
- a heavy engine that cannot be readily handled without the aid of a mechanical hoist may be quickly and accurately dropped into the preassembled position and properly located on the body.
- the assembly is completed merely by tightening the clamping means, which may simply comprise an enlarged head integral with one end of the bolt and an enlarged nut screwed on the other end.
- the mounting described is particularly suitable for use as a front engine mounting, such that similar mountings are employed at opposite forward side portions of the engine with the bolts extending generally longitudinally of the vehicle body.
- the elastic bushing of each assembly is forced into the associated outer tubular member to compress the bushing in the direction of the shorter dimension of the oval cross section, and is provided with diametrically spaced axially extending voids within the larger cross-sectinal dimension.
- the vibration damping and isolating characteristics of a mounting system employing voided bushings are determined by the ratio of the shear rate of the bushing across its voided or longer radial cross sectional dimension to the compression rate of the bushing across its solid or shorter radi' al dimension, and the angular relationship of these radial dimensions relative to the principal inertial axis of the engine. Accordingly the present invention provides simple means for tuning the same bushing assembly effectively for use with vari ous engines and vehicle bodies merely by rotating the axes of the aligned oval holes in the engine bracket into which the bushing assembly is pressed.
- FIG. l is a schematic front elevational view of an engine mounted on a portion of an automobile body in accordance with the present invention.
- FIG. 2 is an enlarged longitudinal sectional view taken in the direction of the arrows substantially along the line 2--2 of FIG. ll.
- F IG. 3 is a transverse sectional view through the bushing assembly, taken in the direction of the arrows substantially along the line 3-3 of FIG. 2.
- FIG. 4 is a fragmentary front elevational view showing the relationship between the engine and body brackets prior to assembly.
- FIG. 5 is a plan view of the structure illustrated in FIG. d.
- an automobile engine 10 is schematically illustrated in FIG. ll mounted on a body crossmember 11 ofa vehicle by means of an engine bracket 12 and body bracket 13 interconnected by a voided bushing assembly 14 at opposite sides of the engine.
- the brackets 12 and 13 are each one-piece steel channel structures described in more detail below, the engine bracket 12 providing means 12a on its channel base for adjustable attachment to the engine 10, as for example by bolts.
- the bracket 13 is likewise suitably secured to the body member 11 in a predetermined position of alignment, as for example by bolts or by welding.
- Each bushing assembly 14 comprises inner and outer steel tubular members 15 and 16 respectively spaced by an elastic bushing 17 of rubberlike material.
- the inner tubular member 15 comprises a tube flattened at diametrically opposite sides lid to provide greater shear resistance within the bushing l7 and has a central axially extending circular opening for the shank of a bolt 19 of a screw threaded clamping means.
- the inner tubular member 15 is suitably bonded to the bushing 17 and may comprise an insert within the molded bushing 117 or may be forced therein after the bushing is molded.
- the outer tubular shell or member 16 has an oval cross section enlarged in the direction of the Hats 18 and is also bonded to the bushing 17 forced therein.
- a thermosetting bonding resin may be applied to the parts to lubricate and facilitate insertion of the bushing 17 under compression into the confines of the outer shell 16. Thereafter the resin is cured to effect the bond.
- Each bushing 17 is compressed in its short radial direction and is relieved in the long radial direction of the flats 18 to provide axially extending voids 21.
- each bushing 17 is provided with an integral annular locating flange 22 at one end which abuts a similar locating flange 23 of the member 16 to facilitate assembly of these members when they are forced together.
- Each of the engine brackets 12 has a pair of axially spaced channel sides 1217 containing a pair of aligned oval openings 120 respectively conforming closely to the outer contour of one of the members 16 to effect an interference fit therewith and to receive the latter when pressed therein, thereby to prevent relative rotation of the bushing assembly 14 within the bracket 12. If desired, the assembled member 16 and bracket channel sides 12b may be further secured against disassembly, as for example by staking.
- each body bracket 13 is provided with a pair of upwardly opening guide slots 1312 respectively adapted to receive the opposite ends of one of the bolts 19 therein.
- the openings of the slots 13b are chamfered at 130 to facilitate downward guided movement of the bolt 19.
- Each channel arm 13a adjacent opposite sides of the opening of its slot 13b is flanged axially outwardly at 13d.
- the bolt 19 is formed with a conventional hexagonal bolthead 19a at one end and is threaded at its opposite end to receive a nut 25.
- a pair of steel washers 26 oversize with respect to the associated slots 13b are provided integrally with the bolthead 1 9a and nut 25 respectively.
- brackets 12 and 13 are properly secured to the engine l and body 11 in their desired fixed positions, with the associated channel sides or elements 12b and 13a spaced axially, or longitudinally of the vehicle body, and with a bushing assembly 14 pressed into and suitably retained within the mating oval holes 12c in each pair of channel sides 1211, a bolt 19 is inserted axially through each of the inner tubular members 15.
- a nut 25 with its integral washer 26 is loosely screwed on the threaded end of each bolt l9,which is adjusted axially within its member 15 so that the nut 25 and bolthead 19a with their respective integral washers 26 will freely clear the flanges 13d, FIG. 4, when the engine is lowered into position, as for example by means of a mechanical hoist.
- the bolt fits closely within the member to avoid play therein and to engage the member 15 frictionally, so as to remain in its adjusted position in the event that during assembly it accidentally strikes one of the bracket arms 13a, for example, or the engine 10 is tilted.
- the opposite ends of the bolts 19 are guided into the chamfered openings 13c and downwardly within the corresponding slots 13b to a preassembled position supported on the bases of the slots.
- the engine will be thus located by the bolts 19 supported on the bases of the slots 13b, whereupon the nuts 25 are tightened to draw the bolts 19 axially from their frictionally retained positions and clamp the washers 26 against the adjacent channel arms 13a, thereby to stress the latter tightly in a positive clamping action against the bushing assembly 14.
- each inner tubular member 15 extends axially beyond the associated outer tubular member 16 and is thus engaged by the channel arms 13a.
- the engine 10 is resiliently supported by the elastic bushing 17 for limited cushioned movement in any direction, whether linear, pivotal, or a combination of such movements.
- the void 21 edgewise of the flat 18 extending in the direction of the roll will be partially closed as the elastic material of the bushing 17 yields to accommodate the roll.
- Engine vibration damping is determined by the relationship of the voids 21 with respect to the solid compressed portion of the bushing 17 along the diameter transverse to the voids 21. It is accordingly apparent that merely by rotating the alignment of the oval holes 12c in the channel sides 12b, the mounting may be readily modified to accommodate minor modifications of the engine or body structure without changing the structure of the bushing assembly 14 or appreciably modifying the mounting brackets 12 and 13. Likewise the same bushing assembly 14 may be employed with different optional engines in the same vehicle body.
- screw threaded clamping means including i. a bolt insertable through said inner tubular member and 2. enlarged clamping members adjustable with. respect to each other on the opposite ends of said bolt,
- bracket elements with axially outwardly directed flanges adjacent the upper openings of said slots and overlying said enlarged clamping members when the latter are clamped tightly against said bracket elements, and prior to locating said engine at said partially assembled position, arranging said bolt within said inner tubular member with said enlarged clamping members spaced axially on said bolt to clear said flanges outwardly thereof when said bolt ends are guided downwardly into said slots.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Transportation (AREA)
- Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
- Vibration Prevention Devices (AREA)
- Connection Of Plates (AREA)
Abstract
Description
Claims (5)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US86072069A | 1969-09-24 | 1969-09-24 | |
US3755670A | 1970-05-15 | 1970-05-15 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3643320A true US3643320A (en) | 1972-02-22 |
Family
ID=26714247
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US37556A Expired - Lifetime US3643320A (en) | 1969-09-24 | 1970-05-15 | Method of mounting an automobile engine |
Country Status (1)
Country | Link |
---|---|
US (1) | US3643320A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5252224U (en) * | 1975-10-13 | 1977-04-14 | ||
JPS5343621U (en) * | 1976-09-20 | 1978-04-14 | ||
US4687188A (en) * | 1986-02-04 | 1987-08-18 | Cooper Tire & Rubber Company | Mount for controlling or isolating vibration |
US6314633B1 (en) * | 1998-09-18 | 2001-11-13 | Illinois Tool Works, Inc. | Method for manufacturing a jounce bumper assembly |
US20080023929A1 (en) * | 2006-07-28 | 2008-01-31 | Daniel R Ryberg | Damped Rear Suspension Track Bar |
US20090060675A1 (en) * | 2007-08-28 | 2009-03-05 | Ford Global Technologies, Llc | A reinforcing sleeve for a tubular beam |
EP2284417A1 (en) * | 2003-06-26 | 2011-02-16 | Lord Corporation | Engine mounts having tuning capabilities and engine decking anti-rotational features |
US11621448B2 (en) * | 2015-01-29 | 2023-04-04 | Ford Global Technologies, Llc | Vehicle frame mounted high voltage battery assembly |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1731540A (en) * | 1929-10-15 | Engine support | ||
US1862483A (en) * | 1930-06-23 | 1932-06-07 | Hugh C Lord | Automobile engine mounting |
US2308458A (en) * | 1940-12-17 | 1943-01-12 | Saurer Curt | Motor mounting |
US2321715A (en) * | 1941-03-22 | 1943-06-15 | Nash Kelvinator Corp | Motor mount |
US2329829A (en) * | 1942-07-27 | 1943-09-21 | Gen Motors Corp | Engine mounting |
US2582040A (en) * | 1948-08-10 | 1952-01-08 | Arthur E Kammritz | Method of installing propeller shaft struts |
US3082999A (en) * | 1959-11-23 | 1963-03-26 | Gen Tire & Rubber Co | Dual rate rubber bushing |
US3432911A (en) * | 1965-02-04 | 1969-03-18 | Rolls Royce | Method and apparatus for installing jet engines |
-
1970
- 1970-05-15 US US37556A patent/US3643320A/en not_active Expired - Lifetime
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1731540A (en) * | 1929-10-15 | Engine support | ||
US1862483A (en) * | 1930-06-23 | 1932-06-07 | Hugh C Lord | Automobile engine mounting |
US2308458A (en) * | 1940-12-17 | 1943-01-12 | Saurer Curt | Motor mounting |
US2321715A (en) * | 1941-03-22 | 1943-06-15 | Nash Kelvinator Corp | Motor mount |
US2329829A (en) * | 1942-07-27 | 1943-09-21 | Gen Motors Corp | Engine mounting |
US2582040A (en) * | 1948-08-10 | 1952-01-08 | Arthur E Kammritz | Method of installing propeller shaft struts |
US3082999A (en) * | 1959-11-23 | 1963-03-26 | Gen Tire & Rubber Co | Dual rate rubber bushing |
US3432911A (en) * | 1965-02-04 | 1969-03-18 | Rolls Royce | Method and apparatus for installing jet engines |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS549779Y2 (en) * | 1975-10-13 | 1979-05-09 | ||
JPS5252224U (en) * | 1975-10-13 | 1977-04-14 | ||
JPS5343621U (en) * | 1976-09-20 | 1978-04-14 | ||
JPS562608Y2 (en) * | 1976-09-20 | 1981-01-21 | ||
US4687188A (en) * | 1986-02-04 | 1987-08-18 | Cooper Tire & Rubber Company | Mount for controlling or isolating vibration |
US6314633B1 (en) * | 1998-09-18 | 2001-11-13 | Illinois Tool Works, Inc. | Method for manufacturing a jounce bumper assembly |
EP2284417A1 (en) * | 2003-06-26 | 2011-02-16 | Lord Corporation | Engine mounts having tuning capabilities and engine decking anti-rotational features |
US20080023929A1 (en) * | 2006-07-28 | 2008-01-31 | Daniel R Ryberg | Damped Rear Suspension Track Bar |
US7648149B2 (en) * | 2006-07-28 | 2010-01-19 | Chrysler Group Llc | Damped Rear Suspension Track Bar |
US7686387B2 (en) | 2007-08-28 | 2010-03-30 | Ford Global Technologies, Llc | Reinforcing sleeve for a tubular beam |
US20100150644A1 (en) * | 2007-08-28 | 2010-06-17 | Ford Global Technologies, Llc | Reinforcing sleeve for a tubular beam |
US20090060675A1 (en) * | 2007-08-28 | 2009-03-05 | Ford Global Technologies, Llc | A reinforcing sleeve for a tubular beam |
US8046918B2 (en) | 2007-08-28 | 2011-11-01 | Ford Global Technologies, Llc | Method for reinforcing a tubular beam with a sleeve |
US11621448B2 (en) * | 2015-01-29 | 2023-04-04 | Ford Global Technologies, Llc | Vehicle frame mounted high voltage battery assembly |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: FIDELITY UNION TRUST COMPANY, TRUSTEE,NEW JERSEY Free format text: MORTGAGE;ASSIGNOR:CHRYSLER CORPORATION;REEL/FRAME:003832/0358 Effective date: 19810209 Owner name: FIDELITY UNION TRUST COMPANY, 765 BROAD ST., NEWAR Free format text: MORTGAGE;ASSIGNOR:CHRYSLER CORPORATION;REEL/FRAME:003832/0358 Effective date: 19810209 |
|
AS | Assignment |
Owner name: CHRYSLER CORPORATION, HIGHLAND PARK, MI 12000 LYNN Free format text: ASSIGNORS HEREBY REASSIGN, TRANSFER AND RELINQUISH THEIR ENTIRE INTEREST UNDER SAID INVENTIONS AND RELEASE THEIR SECURITY INTEREST.;ASSIGNORS:FIDELITY UNION BANK;ARNEBECK, WILLIAM, INDIVIDUAL TRUSTEE;REEL/FRAME:004063/0604 Effective date: 19820217 |
|
AS | Assignment |
Owner name: CHRYSLER CORPORATION Free format text: PARTES REASSIGN, TRANSFER AND RELINQUISH THEIR ENTIRE INTEREST UNDER SAID PATENTS ALSO RELEASE THEIR SECURITY INTEREST.;ASSIGNOR:MANUFACTURERS NATIONAL BANK OF DETROIL (CORPORATE TRUSTEE) AND BLACK DONALD E., (INDIVIDUAL TRUSTEE);REEL/FRAME:004355/0154 Effective date: 19840905 |